Apparatus and method for launch and retrieval of a hovering aircraft

• US 9,434,481 B2
• Filed: 06/26/2014
• Issued: 09/06/2016
• Est. Priority Date: 09/23/2013
• Status: Expired due to Fees

• Current Assignee: Aerovel Corporation (Airbus SE)
• Original Assignee: Aerovel Corporation (Airbus SE)
• Inventors: McGeer, Brian T.
• Primary Examiner(s): Ellis, Christopher P
• Application Number:
  US14/315,899
• Publication Number:
  US 20150239578A1
• Time in Patent Office: 803 Days
• Field of Search: 244/110.F, 244/110.R, 244/110.E, 244/113, 244/63
• US Class Current: 1/1
• CPC Class Codes: B64F 1/0297 adjustable to align with aircraft trajectory
• CPC Class Codes: B64F 1/0299 characterized by the use of multiple devices
• CPC Class Codes: B64F 1/04 for launching aircraft
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 70/30 for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
• CPC Class Codes: B64U 80/10 with means for moving the UAV to a supply or launch location, e.g. robotic arms or carousels
• CPC Class Codes: B64U 80/20 with arrangements for servicing the UAV
• CPC Class Codes: Y10S 901/02 Arm motion controller
• CPC Class Codes: Y10S 901/31 Gripping jaw

Abstract

Various embodiments of the present disclosure provide an apparatus and method for launch and retrieval of a hovering aircraft. Generally, the apparatus of the present disclosure is configured to capture a hovering aircraft between two or more fingers of an aircraft capturer, guide the captured aircraft into a docking station for servicing and/or storage, and launch the aircraft from the docking station. The apparatus of the present disclosure is thus configured to bring the aircraft from an imprecise, irregular hover into a secure and well-controlled rest state. The tolerance of imprecision provided by the apparatus makes it particularly suited for use under a practical conditions such as aboard a small boat in a rough sea.

Claims

1. A method for retrieving an aircraft from free thrust-borne flight, the method comprising:

(a) hovering the aircraft such that a spanwise fixture of the aircraft is positioned over a boom;

(b) sliding a fixture capturer along the boom until the fixture capturer is positioned below the spanwise fixture, the fixture capturer including a first capture member and a second capture member in an open configuration; and

(c) moving the first and second capture members from the open configuration into a closed configuration such that the spanwise fixture is captured between the first and second capture members.

2. The method of claim 1, which includes, after the spanwise fixture is captured between the first and second capture members, sliding the fixture capturer along the boom to position the aircraft in preparation for docking.

3. The method of claim 2, which includes maneuvering the aircraft into a docking station.

4. The method of claim 3, which includes shutting down an engine of the aircraft after the aircraft is in the docking station.

5. The method of claim 1, which includes, while the spanwise fixture is captured between the first and second capture members, rotating at least one of the first and second capture members to draw the aircraft into a designated position relative to the aircraft capturer.

6. A method for launching an aircraft into free thrust-borne flight, the method comprising:

(a) starting an engine of the aircraft;

(b) while a spanwise fixture of the aircraft is captured between first and second capture members of a fixture capturer in a closed configuration, sliding the fixture capturer along the boom to a launch position; and

(c) manipulating the first and second capture members from the closed configuration into an open configuration to release the aircraft into free thrust-borne flight.

7. The method of claim 6, which includes, while the spanwise fixture is captured between the first and second capture members, rotating at least one of the first and second capture members to position the aircraft into a designated position relative to the aircraft capturer.

8. An aircraft retrieval apparatus comprising:

a boom;

a fixture capturer slidably mounted to the boom, the fixture capturer including first and second capture members movable from an open configuration to a closed configuration; and

a controller configured to, while the aircraft is hovering such that a spanwise fixture of the aircraft is positioned over the boom, cause the fixture capturer to slide along the boom until the fixture capturer is positioned below the spanwise fixture and cause the first and second capture members to move from the open configuration to the closed configuration to capture the spanwise fixture therebetween.

9. The apparatus of claim 8, wherein the first and second capture members each include:

(a) a support, (b) a cushioned material at least partially surrounding the support, and (c) a protective coating disposed on an outer surface of the cushioned material.

10. The apparatus of claim 8, further including:

a base; and

a lower arm connected at a first end to the base and at a second end to the boom.

11. The apparatus of claim 8, wherein a first angle separates the first and second capture members when in the open configuration and a second smaller angle separates the first and second capture members when in the closed configuration.

12. The apparatus of claim 8, wherein the first and second capture members are substantially collinear when in the open configuration.

13. The apparatus of claim 8, wherein the first and second capture members are substantially coplanar when in the open configuration.

14. The apparatus of claim 8, wherein the first and second capture members are substantially parallel when in the closed configuration.

15. The apparatus of claim 8, which includes one or more sensors configured to measure the position of the aircraft relative to the fixture capturer.

16. The apparatus of claim 14, wherein the controller is configured to cause the fixture capturer to slide based at least in part on feedback from the one or more sensors.